Shape memory material on the basis of a structural adhesive

Abstract

The present invention relates to a composition comprising a) at least one curable structural adhesive, as well as b) at least one chemically cross-linked elastomer, wherein the elastomer is present as a penetrating polymer network in the structural adhesive. Such a composition constitutes a so-called shape memory material and is suitable for reinforcing cavities in structural components, such as for example in automobile bodies.

Description

Technical field

[0001] The invention lies in the field of compositions comprising curable structural adhesives that are designed as so-called shape memory materials. Furthermore, the invention relates to a reinforcing element for reinforcing cavities in structural components, such as those used in automobile bodies and the like. State of the art

[0002] Hollow structural components are often used in all types of construction. This design allows for the weight of the structure and the use of materials to be kept low, but this construction method often results in a loss of stability and strength. Furthermore, due to the larger surface area of ​​the hollow component, the cavities offer a larger surface area for corrosion if moisture or dirt penetrates them. Noise caused by wind or vibrations, for example, can also be transmitted in or along the cavities. Due to the shape and / or narrow dimensions of such cavities, it is often difficult to effectively reinforce, seal, or contain noise transmission.

[0003] In particular, to improve the mechanical properties of hollow structural components, it is common practice to insert or incorporate local reinforcement elements into the components. Such reinforcement elements are typically made of metals or plastics, or combinations of these materials. Structural foams are also frequently used in hard-to-reach areas that, for example, need to be reinforced or sealed after the component has been assembled. This is the case, for example, in the manufacture of vehicle structures or car bodies. The advantage of structural foams is that they can be installed in a cavity in an unexpanded state and later foamed, especially by increasing the temperature.For example, the inner wall of the cavity can be fully coated using cathodic dip coating (CDP) even after the reinforcement element has been installed, and only then reinforced by foaming the structural adhesive. Foaming typically occurs during the curing of the CDP layer in the oven.

[0004] The disadvantage of such reinforcing elements is that the mechanical properties of the structural adhesive are impaired during the foaming process. Description of the invention

[0005] The object of the present invention is therefore to provide a reinforcing element which overcomes the disadvantages of the prior art and allows a gap between the cavity and the reinforcing element to be closed without impairing the mechanical properties of the structural adhesive.

[0006] Surprisingly, it has been found that this object can be achieved with compositions according to claim 1.

[0007] It has been found that compositions according to the invention can be used to produce shape memory materials which change their shape, in particular due to the influence of temperature, and thus expand in a desired direction without being accompanied by an increase in volume, for example due to a foaming process.

[0008] Further aspects of the invention are the subject of further independent claims. Particularly preferred embodiments of the invention are the subject of the dependent claims. Short description of the drawings

[0009] Embodiments of the invention are explained in more detail with reference to the drawings. Identical elements are provided with the same reference numerals in the various figures. Naturally, the invention is not limited to the embodiments shown and described.

[0010] They show: Figure 1 a schematic representation of the production of a shaped body or a composition in its temporary form; Figure 2 a schematic representation of the reinforcing element; Figure 3 a schematic representation of the shape change and curing of the composition; Figure 4 a schematic representation of the reinforcement of a cavity of a structural component; Figure 5 a schematic representation of a reinforcing element in a cavity of a structural component; Figure 6 a schematic representation of a reinforced structural component.

[0011] The figures show only the elements essential for a direct understanding of the invention. Ways to implement the invention

[0012] The present invention relates in a first aspect to a use of a composition comprising i) at least one curable structural adhesive; and ii) at least one chemically cross-linked elastomer; where the chemically cross-linked elastomer is present as a penetrating polymer network in the structural adhesive, as a shape memory material.

[0013] The term "interpenetrating polymer network" is used in this document based on the definition of a "semi-interpenetrating polymer network" (SIPN) according to the IUPAC Compendium of Chemical Terminology, 2nd Edition (1997). Accordingly, the SIPN comprises at least one network and at least one linear or branched polymer, with this polymer at least partially penetrating the network. In the composition, the elastomer forms the network, and the polymer is a component of the curable structural adhesive.

[0014] In this document, "chemically crosslinked elastomer" refers to an elastomer that is crosslinked via covalent chemical bonds. In contrast, the crosslinking of a thermoplastic elastomer is based on physical interactions. A chemically crosslinked elastomer differs from a thermoplastic elastomer in that it swells in a suitable solvent but does not dissolve. A thermoplastic elastomer, on the other hand, dissolves completely in a suitable solvent. The presence of a chemically crosslinked elastomer can be determined, for example, based on ASTM D 2765.

[0015] In this document, the glass transition temperature T g of a composition is defined as the glass transition temperature of the curable structural adhesive, in particular the epoxy resin A,or the glass transition temperature of the chemically crosslinked elastomer, whichever is higher. In embodiments with a curable structural adhesive based on a solid epoxy resin, the glass transition temperature T g of the composition generally refers to the glass transition temperature T g of the solid epoxy resin. In embodiments with a curable structural adhesive based on a liquid epoxy resin, the glass transition temperature T g of the composition generally refers to the glass transition temperature T g of the chemically crosslinked elastomer. The glass transition temperature T g and melting points are typically measured using DSC (Differential Scanning Calorimetry). The measurements are carried out on 5 mg samples using a Mettler Toledo 822e instrument at a heating rate of 10°C / min up to 180°C. The measured values ​​are determined from the measured DSC curve using DSC software.

[0016] The composition, which constitutes a "shape memory material," can be formed into a specific shape ("original shape") during its production or processing. After this shaping, it exhibits a solid consistency, meaning that the composition exists at a temperature below its glass transition temperature Tg. In this form, the chemically crosslinked elastomer, which is present as a pervasive polymer network in the structural adhesive, is essentially relaxed. If necessary, the composition is then heated to a temperature above its glass transition temperature Tg and formed into any desired shape ("temporary shape"). In this temporary form, the chemically crosslinked elastomer exists in a stressed state.The composition is held in this temporary form, and its temperature is lowered back below its glass transition temperature Tg, causing the composition to solidify in the temporary form. In this temporary form, the composition is storage-stable and can be subjected to processing, such as punching or cutting. If the composition is later heated to a temperature above its glass transition temperature Tg, the elastomer returns to its relaxed shape, thus deforming the entire composition to its original form.

[0017] In particular, the composition is a shape memory material which is solid at room temperature (23°C), allowing optimal handling of the material in its original and temporary form.

[0018] For the composition to be solid at room temperature, it should have a glass transition temperature T g above room temperature. Otherwise, once the composition has been formed into its temporary shape, the elastomer strained in this temporary shape would not be able to retain this shape at room temperature.

[0019] The composition preferably has a glass transition temperature T g in the range from 23°C to 95°C, in particular from 30°C to 80°C, preferably from 35°C to 75°C.

[0020] Further preferably, the surface of the composition is non-sticky at room temperature, which facilitates its handling.

[0021] The curable structural adhesive is in particular a heat-curing structural adhesive which preferably has a curing temperature in the range of 120°C to 220°C, in particular 160°C to 200°C.

[0022] If the curable structural adhesive is a heat-curing structural adhesive, care must be taken during processing of the composition, in which it is brought into its temporary form, to ensure that the composition is not heated to such an extent that the curing process begins.

[0023] Most preferably, the curable structural adhesive is an epoxy resin composition comprising at least one epoxy resin A and at least one hardener B for epoxy resins, which is activated by elevated temperatures. Specifically, it is a one-component epoxy resin composition.

[0024] The epoxy resin A,has an average of more than one epoxy group per molecule and is, in particular, a solid epoxy resin or a mixture of a solid epoxy resin with a liquid epoxy resin. The term "solid epoxy resin" is well known to epoxy experts and is used in contrast to "liquid epoxy resin." The glass transition temperature T g of solid resins is above room temperature.

[0025] Preferred solid epoxy resins have the formula (I).

[0026] Here, the substituents R' and R" independently of one another represent either H or CH 3 . Furthermore, the index s represents a value of ≥ 1, in particular ≥ 1.5, preferably from 2 to 12.

[0027] Preferred solid epoxy resins have a glass transition temperature T g in the range from 23°C to 95°C, in particular from 30°C to 80°C, preferably from 35°C to 75°C.

[0028] Such solid epoxy resins are commercially available, for example, from Dow Chemical Company, USA, from Huntsman International LLC, USA, or from Hexion Specialty Chemicals Inc, USA.

[0029] Preferred liquid epoxy resins, which can be used in particular together with a solid epoxy resin, have the formula (II).

[0030] Here, the substituents R'" and R"" independently of one another represent either H or CH 3 . Furthermore, the index r represents a value from 0 to 1. Preferably, r represents a value of ≥ 0.2.

[0031] These are therefore preferably diglycidyl ethers of bisphenol A (DGEBA), bisphenol F, and bisphenol A / F. The designation "A / F" refers to a mixture of acetone with formaldehyde, which is used as a starting material in its production. Such liquid resins are commercially available, for example, under the trade names Araldite ®< GY 250, Araldite ®< PY 304, Araldite ®< GY 282 from Huntsman International LLC, USA, or DER ®< 331 or DER ®< 330 from Dow Chemical Company, USA, or under the trade names Epikote ®< 828 or Epikote ®< 862 from Hexion Specialty Chemicals Inc, USA.

[0032] Depending on the embodiment, the epoxy resin used as one of the starting compounds in the curable structural adhesive can also be a liquid epoxy resin. This is typically the case when the curable structural adhesive comprises at least one chemically crosslinked elastomer to form a shape memory material. The chemical crosslinking of the polymeric constituents used to produce this elastomer, i.e., the elastomer-building components, leads to an increase in the glass transition temperature T g of the composition, so that it lies within a range suitable for handling the material. This is the case, for example, when the chemically crosslinked elastomer is constructed at least partially from the liquid epoxy resin used.

[0033] Other suitable epoxy resins are so-called novolaks. These have, in particular, the following formula (III).

[0034] The radical X represents a hydrogen atom or a methyl group. The radical Y represents -CH 2 - or a radical of formula (IV).

[0035] Furthermore, the index z stands for a value from 0 to 7, in particular for a value of ≥ 3.

[0036] In particular, these are phenol or cresol novolaks (Y stands for -CH 2 -).

[0037] Such epoxy resins are commercially available under the trade names EPN or ECN as well as Tactix ®< 556 from Huntsman International, LLC, USA, or under the product line DEN ™< from Dow Chemical Company, USA.

[0038] Preferably, the epoxy resin A a solid epoxy resin of the formula (I). In a likewise preferred embodiment, the heat-curing epoxy resin composition contains both at least one solid epoxy resin of the formula (I) and at least one liquid epoxy resin of the formula (II).

[0039] The proportion of epoxy resin A is preferably 2 to 90 wt.%, in particular 5 to 70 wt.%, preferably 10 to 60 wt.%, based on the total weight of the curable structural adhesive.

[0040] The Hardener B for epoxy resins is activated by elevated temperature. The hardener is preferably B a hardener selected from the group consisting of dicyandiamide, guanamines, guanidines, aminoguanidines and their derivatives; substituted ureas, in particular 3-(3-chloro-4-methylphenyl)-1,1-dimethylurea (chlorotoluron), or phenyl-dimethylureas, in particular p-chlorophenyl-N,N-dimethylurea (monuron), 3-phenyl-1,1-dimethylurea (fenuron), 3,4-dichlorophenyl-N,N-dimethylurea (diuron), as well as imidazoles and amine complexes.

[0041] Particularly preferred as a hardener Bis dicyandiamide, especially in combination with a substituted urea. The advantage of combining dicyandiamide with a substituted urea is the resulting accelerated curing of the composition.

[0042] The proportion of hardener B is preferably 0.05 to 8 wt.%, in particular 0.1 to 6 wt.%, preferably 0.2 to 5 wt.%, based on the total weight of the curable structural adhesive.

[0043] The term "hardener" in this document also includes catalysts and catalytically active compounds. In this case, it is clear to the person skilled in the art that when using a catalyst or a catalytically active compound as a hardener B, the proportion of hardener B of the entire curable structural adhesive is in the lower range of the specified value range.

[0044] Additionally, the epoxy resin composition may comprise at least one impact modifier.

[0045] In this document, an "impact modifier" is understood to mean an addition of an organic polymer to an epoxy resin matrix which, even in small amounts, i.e. typically between 0.1 and 20 wt.%, causes a significant increase in toughness and is thus able to absorb higher impact or shock loads before the matrix tears or breaks.

[0046] Particularly suitable impact modifiers are reactive liquid rubbers based on nitrile rubber or derivatives of polyether polyol polyurethanes, core-shell polymers and similar systems known to the person skilled in the art.

[0047] Suitable impact modifiers are known as impact modifiers Ddescribed in European patent application number EP08168009.2, the contents of which are hereby incorporated by reference.

[0048] The curable structural adhesive may contain other components commonly used in curable structural adhesives.

[0049] In particular, the curable structural adhesive additionally contains at least one filler. These are preferably mica, talc, kaolin, wollastonite, feldspar, syenite, chlorite, bentonite, montmorillonite, calcium carbonate (precipitated or ground), dolomite, quartz, silica (pyrogenic or precipitated), cristobalite, calcium oxide, aluminum hydroxide, magnesium oxide, hollow ceramic spheres, hollow glass spheres, organic hollow spheres, glass spheres, and color pigments. Fillers include both the organically coated and uncoated forms that are commercially available and known to those skilled in the art. Another example is functionalized alumoxanes, as used, for example, in

[0050] US 6,322,890, the contents of which are hereby incorporated by reference.

[0051] Advantageously, the proportion of filler is 1 to 60 wt.%, preferably 5 to 50 wt.%, in particular 10 to 35 wt.%, based on the weight of the total curable structural adhesive.

[0052] As further components, the curable structural adhesive also comprises, in particular, thixotropic agents such as aerosils or nanoclays, toughness modifiers, reactive diluents and other components known to the person skilled in the art.

[0053] Typically, the composition does not contain any chemical blowing agent or any other agent that causes the composition to foam.

[0054] Most preferably, the curable structural adhesive is a one-component, heat-curing epoxy resin composition.

[0055] The composition comprises at least one chemically cross-linked elastomer which is present as a penetrating polymer network in the structural adhesive.

[0056] The chemically cross-linked elastomer is introduced into the composition by mixing elastomer-building components with the curable structural adhesive and then cross-linking them in the mixture to create a permeating polymer network in the structural adhesive.

[0057] Any components that can be crosslinked in a controlled manner to form an elastomer when mixed with the curable structural adhesive can be used as elastomer building components without impairing the function of the curable structural adhesive.

[0058] In particular, the elastomer-building components are selected from the group consisting of at least one natural or synthetic rubber and at least one crosslinking agent for rubber; and at least one polyisocyanate and at least one polyol.

[0059] In addition to natural rubber, i.e. polyisoprene, synthetic rubbers such as styrene-butadiene rubber, polybutadiene rubber, acrylonitrile-butadiene rubber, especially with an acrylonitrile content of ≥ 25 mol-%, chloroprene rubber and ethylene-propylene-diene rubber are typically suitable.

[0060] The crosslinking can be carried out with sulfur, radically or in another manner known to the person skilled in the art.

[0061] Furthermore, the elastomer-building components can be polyisocyanates and polyols, as are well known to those skilled in the art. In particular, the polyisocyanates are commercially available diisocyanates such as diphenylmethane diisocyanate (MDI), tolylene diisocyanate (TDI), 1,6-hexamethylene diisocyanate (HDI), or 1-isocyanato-3,3,5-trimethyl-5-isocyanatomethylcyclohexane (IPDI).

[0062] The polyols are, in particular, polymeric polyols, especially di- or trifunctional polyols. Suitable polymeric polyols are typically polyether polyols, polyester polyols, polycarbonate polyols, and mixtures of these polyols. In particular, the polymeric polyols have a molecular weight in the range of 500 to 5000 g / mol.

[0063] During the preparation of the composition, the curable structural adhesive is mixed with elastomer components until a homogeneous mixture is obtained. The curable structural adhesive comprises an epoxy resin. A a solid epoxy resin, mixing takes place at a temperature above the glass transition temperature T g of the solid epoxy resin. If the curable structural adhesive is a heat-curing epoxy resin composition, this can be Bwith the elastomer components. This allows the mixing temperature to be adjusted to or even above the curing temperature of the heat-curing epoxy resin composition without curing the structural adhesive. Higher temperatures generally result in more efficient mixing.

[0064] After a homogeneous mixture has been obtained, the elastomer-building components are crosslinked to form an elastomer, which is present as a penetrating polymer network in the structural adhesive.

[0065] The proportion of chemically crosslinked elastomer is preferably 1 to 40 wt.%, in particular 10 to 20 wt.%, based on the total weight of the composition.

[0066] In a preferred embodiment of the present invention, the chemically crosslinked elastomer is constructed from components of the curable structural adhesive.

[0067] In this embodiment, the composition comprises a chemically crosslinked elastomer which is present as a penetrating polymer network in the structural adhesive, which is composed of epoxy resin A and at least one additional hardener H for epoxy resins.

[0068] The Hardener H is a molecule or polymer that contains functional groups reactive with epoxy groups, particularly with an average functionality of > 2 to 5 and an average equivalent weight of 40 to 2000 g / eq. Functionality is understood to mean functionality toward epoxy groups.

[0069] Furthermore, the activation temperature of the hardener H below the activation temperature of the hardener B, which is described above. Preferably, the activation temperature of the hardener is Hat least 10°C, in particular at least 20°C, preferably at least 30°C, below the activation temperature of the hardener B.

[0070] Furthermore, the stoichiometric ratio of the sum of the reactive groups of hardener H and hardener B to the epoxy groups of the epoxy resin A in the range of ≥ 0.9:1.

[0071] When hardening H It is a molecule or a polymer that has functional groups reactive with epoxy groups. Typically, it is a polymer, and this polymer is selected in particular from the group consisting of polyolefin, polyether, polyester, fatty acid, fatty acid amide, and acrylonitrile-butadiene rubber with an acrylonitrile content of ≥ 25 mol%.

[0072] For the present invention it is important that the hardener Hhas a basic structure which does not differ from the rest of the composition, in particular from the epoxy resin A segregated, as do known elastomers that are usually added to epoxy resin compositions as impact modifiers. This would be the case, for example, with acrylonitrile-butadiene rubber with a low acrylonitrile content, particularly below 25 mol%.

[0073] Typically, such hardeners are H flexibilizing.

[0074] In the case of the functional groups of the hardener that are reactive with epoxy groups HThese are, in particular, amino, carboxyl, carboxylamide, hydroxyl, or anhydride groups. They are preferably amino or carboxyl groups or phenolic hydroxyl groups, preferably amino or carboxyl groups. Carboxyl groups are particularly preferred because the composition can then be cured after crosslinking with the hardener H, but before crosslinking with the hardener B, has better storage stability. The reason for this is that reacted amines, which are thus present in the composition as tertiary amines, can catalyze the homopolymerization of the epoxy groups.

[0075] The average functionality of the polymer is in the range from > 2 to 5, in particular from 2.5 to 5, preferably from 3 to 5. The average equivalent weight of the polymer is in the range from 40 to 1000 g / Eq, in particular from 40 to 1000, preferably from 50 to 800. The equivalent weight is the ratio of the molecular weight of the entire polymer, ie the hardener H, to its functionality, ie the number of functional groups reactive with epoxide groups,

[0076] Most preferred is the hardener Hdiamines such as 4,9-dioxadodecane-1,12-diamine or polyetherpolyamines, as are commercially available, for example, under the trade name Jeffamine ®< , in particular as Jeffamine ®< D-230 or T-403, from Huntsman International LLC, USA, or dimer or trimer fatty acids, as are commercially available, for example, under the trade name Pripol ™< , in particular Pripol ™< 1040, from Croda International PLC, England.

[0077] The Hardener B, which is also used in this preferred embodiment of the composition according to the invention, has already been described above.

[0078] In particular, the stoichiometric ratio of the reactive groups of hardener H to the reactive groups of hardener B in the range of ≥ 1:1.

[0079] It is essential for the composition according to the invention that it be designed as a shape memory material, which has the highest possible dimensional stability in the temporary shape and the most complete possible recovery capacity. In concrete terms, this means that the composition according to the invention is able to retain its temporary shape for the longest possible period of time, typically for longer than 6 months, and that the composition, if necessary, completely returns to its original shape by heating above the glass transition temperature T g of the composition. Adequate recovery capacity is typically present when a test specimen made from a composition according to the invention with a height in the range of 5 to 10 mm is deformed by 50% in height and can be returned to 80 to 100% of its original height if necessary.

[0080] In the preferred embodiment of the present invention, where the composition comprises a chemically crosslinked elastomer composed of epoxy resin A and at least one hardener H For epoxy resins, this means that the crosslinking of the epoxy resin A with the hardener H must bring about these properties.

[0081] However, it is important to ensure that the crosslinking of the remaining epoxy groups of the epoxy resin A with the hardener B sufficient adhesion of the structural adhesive. Ideally, in this embodiment, the proportion of hardener H in the composition only just enough to obtain a shape memory material with the said properties, so that as many epoxy groups of the epoxy resin A as possible, for curing with the hardener B, i.e. for the development of adhesion.

[0082] The composition, which represents the preferred embodiment, is prepared in a process comprising the steps: Mixing the epoxy resin A with at least one hardener B; Addition and mixing of a hardener H; Implementing the epoxy resin A with the hardener H; or mixing the epoxy resin A with at least one hardener H and a hardener B; Implementing the epoxy resin A with the hardener H at a temperature below the activation temperature of the hardener B.

[0083] In particular, the hardener Ha hardener which reacts with the epoxy resin at room temperature or at a significantly lower temperature than hardener B, whereby no or only little energy in the form of heat needs to be supplied to produce the composition according to the invention, i.e. a shape memory material.

[0084] A further aspect relates to a shaped body which has been subjected to reversible shaping, wherein the shaping comprises the steps: 1. a) heating a composition as previously described to a temperature above its glass transition temperature T g ; 2. b) deforming the composition, while stressing the chemically crosslinked elastomer; 3. c) cooling the deformed composition below its glass transition temperature T g .

[0085] Figure 1shows schematically the production of a shaped body from a composition based on an epoxy resin composition as previously described.

[0086] The solid composition 1 is in its initial state Z1 in the original form in which it was brought, for example, during its production. In a first step, the composition is then heated by a temperature ΔT 1 to a temperature which is above its glass transition temperature T g, but, in the case of a heat-curing epoxy resin composition, below its curing temperature. Once the composition is in this state Z2, it is brought into its temporary, still deformable form 2 under the action of a force F. In this temporary, still deformable form, as shown in state Z3, the chemically cross-linked elastomer is in a tensioned form. The composition is held in this temporary form and the temperature of the composition is again reduced by the temperature ΔT 1 to a temperature which is below its glass transition temperature T g.The composition solidifies and is now in its temporary form 3, as shown in state Z4. In this state, as a molded body, the composition is storage-stable and can be further processed. The molded body can be punched or cut and / or, in particular, attached to a support or arranged in a cavity of a structural component to be reinforced.

[0087] The deformation of the composition, which involves bringing it into its temporary shape, is typically carried out by pressing, rolling, drawing, etc. It is important during deformation that the composition can be cooled in the deformed state to a temperature below its glass transition temperature T g so that it remains in its temporary shape.

[0088] In a further aspect, the present invention relates to a reinforcing element for reinforcing cavities in structural components comprising a carrier to which a shaped body according to the above description is attached.

[0089] This carrier can be made of any material. In particular, the carrier consists of a plastic, a metal, or a combination of plastic and metal.

[0090] Preferred plastics are polyurethanes, polyamides, polyesters, and polyolefins and polyolefin copolymers, especially high-temperature-resistant polymers such as poly(phenylene ether), polysulfones, or polyethersulfones. Most preferred plastics are polyamides (PA) such as PA6 or PA66, polyethylene and polypropylene, as well as polystyrene and copolymers such as acrylonitrile butadiene styrene (ABS). Preferred metals are aluminum, steel, nickel, and alloys of these metals. The metal can be untreated or pretreated with suitable agents, for example, to prevent corrosion or improve adhesion.

[0091] The carrier can also have any desired structure and design. For example, it can be solid, hollow, foamed, or have a grid-like structure. The surface of the carrier can typically be smooth, rough, or textured.

[0092] In addition to its function as a support for the composition or the molded part made from it, the carrier can contribute to structural reinforcement or sealing of the component or even to sound insulation.

[0093] The carrier can further comprise at least one fastening means, in particular a clip, for securing and positioning the reinforcement element in a cavity. Securing the reinforcement element with a clip is particularly suitable for applications in which the entire surface of the component, including the cavity's inner wall, must be accessible, for example, for dip coating. In such cases, fastening by adhesive, for example, is not suitable, since the paint cannot reach the bonding point.

[0094] Most preferably, the carrier consists of a plastic coated with a metal. The previously described materials are preferred as the plastic and the metal.

[0095] The metal with which the plastic is coated can be attached to the plastic in any desired manner. For example, the attachment is achieved by mechanical fasteners such as nails, screws, rivets, mechanical clips, clamps, crimps, and the like, or by gluing the metal to the plastic. Furthermore, the metal can also be applied to the plastic by means of plastic electroplating. The thickness of the metal layer on the plastic carrier is usually between 0.03 and 1.5 mm.

[0096] A metal-coated plastic substrate has the advantage over a pure metal substrate that it is lighter and, thanks to the properties of the plastic, such as the choice of material and its processing, its mechanical properties and design can be varied very widely. The advantage of a metal coating over a pure plastic substrate is that metals generally bond better. A further advantage of a metal coating is that, with heat-curing structural adhesives, the metal layer can be heated very locally and efficiently by induction.

[0097] Figure 2 shows a carrier 5 made of a plastic, which is coated with a metal 8. The metal is attached to the carrier with nails 9. On the metal layer is a molded body 3 consisting of a composition in its temporary state.

[0098] Figure 3 shows schematically a reinforcing element consisting of a carrier 5, to which a molded body 3 made of a composition with a heat-curing epoxy resin composition as a structural adhesive and a chemically crosslinked elastomer in its temporary form is attached, in its initial state Z4. In a first step, the molded body 3 is then heated by a temperature ΔT 1 to a temperature which is above the glass transition temperature T g of the composition, whereby the elastomer relaxes and leads to a deformation of the molded body or the composition 1 into its original shape. This corresponds to state Z5 in Figure 3 . The temperature is then further increased by ΔT 2 to a temperature at which the composition cures. The cured composition 4 is shown in state Z6.

[0099] The temperature increase that leads to the deformation of the molded body and the temperature increase that cures the structural adhesive do not necessarily have to occur in two stages. It is certainly possible to perform the two steps sequentially by continuously increasing the temperature.

[0100] The invention further encompasses the use of a reinforcing element as described above for reinforcing cavities in structural components. Such structural components are preferably used in bodies and / or frames of means of transport and locomotion, in particular waterborne or land-based vehicles or aircraft. The invention preferably encompasses the use of a reinforcing element in bodies or frames of automobiles, trucks, railway carriages, boats, ships, helicopters, and aircraft, most preferably in automobiles.

[0101] A further aspect relates to a method for reinforcing cavities in structural components comprising the steps: a') Placing a reinforcing element as described above into the cavity of a structural component; b') Heating the molded body 3 on the reinforcing element to a temperature above the glass transition temperature T g of the composition, whereby the molded body returns to its pre-molding shape, i.e. to its original shape; c') Curing the curable structural adhesive.

[0102] In one embodiment of the described method for reinforcement in cavities of structural components, in which the proviso applies that the carrier of the reinforcing element consists of a metal that can be heated by induction or of a material that is coated with a metal that can be heated by induction, and with the proviso that the curable structural adhesive is a heat-curing structural adhesive, steps b') and c') are effected by induction, that is to say by an alternating electromagnetic field of an induction coil.

[0103] Figure 4 shows analogous to Figure 3schematically the reinforcement in a cavity of a structural component 6, wherein a reinforcing element consisting of a carrier 5 and several molded bodies 3 made of a composition with heat-curing structural adhesive and chemically cross-linked elastomer in their temporary form is attached inside the structural component. The carrier of the reinforcing element is fastened to the structural component with a clip 7. The molded body or the composition is in its temporary form (state Z4) and is subsequently heated by a temperature ΔT 1 to a temperature which is above the glass transition temperature T g of the composition. The elastomer relaxes and leads to a deformation of the molded body or the composition 1 into its original shape, whereby the gap 10 left open between the reinforcing element and the cavity is closed and the composition adheres to the inner wall of the cavity (state Z5).After a further temperature increase by a temperature ΔT 2, the heat-curing structural adhesive cures. Figure 4 , Condition Z6, shows the reinforced structural component with the cured composition 4.

[0104] Figure 5 shows a reinforcing element as it is inserted into a cavity 10 of a structural component 6 before the deformation of the shaped body or the composition in its temporary form 3, which is located on a carrier 5.

[0105] Figure 6 shows the reinforcement element from Figure 5 as it is inserted into a cavity of a structural component 6, wherein the molded part or the composition in this case has already returned to its original shape and adheres to the inner walls of the structural component 6. Furthermore, Figure 6 the cured composition 4. The shape and structure of the reinforcing elements can be freely selected according to their place of use.

[0106] Furthermore, the present invention relates to a cured composition as obtainable by a curing process, in particular by heat curing, from a previously described composition. Examples

[0107] The following are exemplary embodiments intended to illustrate the described invention in more detail. Of course, the invention is not limited to these described exemplary embodiments. Test procedures

[0108] The dimensional stability The material in the temporary form was tested for 7 days at standard climate (23°C / 50% humidity) ( "Relaxation" ), the resilience to the original shape after 7 days of storage under standard conditions. The dimensions of the original shape of the test specimens are 10x10x6 mm (LxWxH). The height in original shape ( H 0 ) was 6 mm. By pressing at elevated temperature and subsequent cooling, the test specimens were brought into the temporary shape with a height of 3 mm ( H Temp ), which corresponds to a compression of 50% and thus allows a height gain of 100% during the reset process.

[0109] The relaxation is defined here as: Relaxation % = H Temp Tag 7 − H Temp Tag 0 H Temp Tag 0 ⋅ 100

[0110] The resilience is determined as: Rückstellvermögen % = H 0 Tag 7 , nach Aushärtung H 0 Tag 0 ⋅ 100 Production of the test specimens

[0111] The examples 1 and 2 represents a structural adhesive based on an epoxy resin composition and a chemically crosslinked elastomer, which is composed of components of the epoxy resin.

[0112] The formulations 1 and 2 were prepared by mixing the components according to Table 1 in the corresponding weight percentages using a speed mixer at 40°C.

[0113] The formulations 3 until 6 and the reference foam Ref were prepared by mixing the components according to Table 2 in the corresponding weight percentages on a twin-screw extruder at a temperature above the glass transition temperature T g of the solid resin or below the decomposition temperature of the chemical blowing agent ( Ref ).

[0114] In the examples 5 and 6 The polyols were reacted with the diisocyanate and, if appropriate, with the catalyst before being mixed into the respective formulation, in a process known to the person skilled in the art, to form a polyurethane polymer containing isocyanate groups.

[0115] The resulting formulations were processed into test specimens in their original form measuring 10 x 10 x 6 mm. The respective elastomers were then chemically crosslinked at 90°C for one hour. 1 3 Ref Table 1 Formulations up to and reference foam in wt% and results; Ref 1 2 Araldite ®< GT 7004 a)< 85.4 Araldite ®< GY 250 a)< 77.2 60 Dicyandiamide b)< 1.6 1.5 1.1 Jeffamine ®< D-230 a)< 13.5 Armies ®< CD c)< 7.8 Pripol ™< 1040 d)< 14.2 Bisphenol A e)< 21.9 PPh 3 e)< 2.8 Luvopor ®< OB f)< 3 Aerosil ® g)< 10 Relaxation [%] - 5 0 Recovery capacity [%] - 100 100 a)< available from Huntsman Advanced Materials (Switzerland); b)< available from AlzChem GmbH, Germany; c)< available from Akzo Nobel GmbH, Sweden; d)< available from Croda Inc., UK; e)< available from Fluka, Switzerland; f)< available from Lehmann&Voss&Co, Germany; g)< available from Wacker Chemie AG, Germany. 3 6 Table 2 Formulation up to wt% and results; 3 4 5 6 Araldite ®< GT 7004 73 63 64 64 Dicyandiamide 1.5 1.2 1.2 1.2 Nipol ®< 1072 (rubber) a)< 20 30 Dibenzoyl peroxide b)< 0.6 0.6 Desmophen ®< 3060 BS (polyol) c)< 14 Acclaim ®< 4200 (Polyol) c)< 14 24.37 Takenate ®< 500 (polyisocyanate) d)< 4 Desmodur ®< 3400 (polyisocyanate) c)< 7.7 Dibutyltin dilaurate 0.03 Purmol ®< 13 e)< 1.6 1.6 Aerosil ®< 5 5 1 1 Relaxation [%] 0 0 0 0 Recovery capacity [%] 80 95 75 50 a)< available from Zeon Chemicals, USA; b)< available from Arkema, France; c)< available from Bayer MaterialScience, Germany; d)< available from Mitsui Chemicals, Japan; e)< available from Zeochem AG, Switzerland. List of reference symbols

[0116] 1Composition in its original form 2Composition (deformable) 3Form body (temporary form) 4Cured composition 5Support 6Structural component 7Clip 8Metal layer 9Nail 10Gap Z1State of the composition in its original form Z2State of the deformable composition Z3State of the composition in its temporary state (form body) Z4State of the cured composition ΔT 1 Temperature difference between temperature below T g of the composition and temperature above T g of the composition ΔT 2 Temperature difference between temperature above T g of the composition and the curing temperature of the composition

Claims

1. Use of a composition comprising i) at least one curable structural adhesive; and ii) at least one chemically cross-linked elastomer; characterized in that the chemically cross-linked elastomer is present in the structural adhesive as a penetrating polymer network, as a shape memory material.

2. Use of the composition according to Claim 1, characterized in that the curable structural adhesive is a thermosetting epoxy resin composition comprising at least one epoxy resin A and at least one hardener B for epoxy resins which is activated by elevated temperature.

3. Use of the composition according to either of the preceding claims, obtainable by - mixing at least one curable structural adhesive with elastomer-building components; - cross-linking the elastomer-building components in the mix to an elastomer so that a penetrating polymer network is formed in the structural adhesive.

4. Use of the composition according to Claim 3, characterized in that the elastomer-building components are selected from the group consisting of - at least one natural or synthetic rubber and at least one cross-linking agent for rubber; and - at least one polyisocyanate and at least one polyol.

5. Use of the composition according to Claim 2, characterized in that the chemically cross-linked elastomer, which is present in the structural adhesive as penetrating polymer network, is built from epoxy resin A and at least one additional hardener H for epoxy resins, - wherein the hardener H is a molecule or polymer, which has functional groups reacting with epoxide groups having a medium functionality of > 2 to 5 and a mean equivalence weight of 40 to 2000 g / eq; - wherein the activation temperature of the hardener H is below the activation temperature of the hardener B; and - wherein the stoichiometric ratio of the sum of the reactive groups of hardener H and hardener B to the epoxide groups of the epoxy resin A is in the range of ≥ 0.9:1.

6. Use of the composition according to Claim 5, characterized in that the stoichiometric ratio of the reactive groups of hardener H to the reactive groups of hardener B is in the range of ≥ 1:1.

7. Use of the composition according to Claim 5, characterized in that the hardener H is a polymer having amino or carboxyl groups, wherein the polymer is selected from the group consisting of polyolefin, polyether, polyester, fatty acid, fatty acid amide and acrylonitrile-butadiene rubber with an acrylonitrile proportion of ≥ 25 mol%.

8. Use of the composition according to Claim 7, characterized in that the hardener H is a polyether polyamine.

9. Use according to Claim 5, characterized in that the composition is obtainable by a method comprising the steps of: - mixing the epoxy resin A with at least one hardener B; - adding and admixing a hardener H; - reacting the epoxy resin A with the hardener H; or - mixing the epoxy resin A with at least one hardener H and one hardener B; - reacting the epoxy resin A with the hardener H at a temperature below the activation temperature of hardener B.

10. Composition comprising i) at least one curable structural adhesive; and ii) at least one chemically cross-linked elastomer; wherein the chemically cross-linked elastomer is present in the structural adhesive as a penetrating polymer network, characterized in that the curable structural adhesive is a thermosetting epoxy resin composition comprising at least one epoxy resin A and at least one hardener B for epoxy resins which is activated by elevated temperature, and in that the chemically cross-linked elastomer, which is present in the structural adhesive as penetrating polymer network, is built from epoxy resin A and at least one additional hardener H for epoxy resins, - wherein the hardener H is a molecule or polymer, which has functional groups reacting with epoxide groups having a medium functionality of > 2 to 5 and a mean equivalence weight of 40 to 2000 g / eq; - wherein the activation temperature of the hardener H is below the activation temperature of the hardener B; and - wherein the stoichiometric ratio of the sum of the reactive groups of hardener H and hardener B to the epoxide groups of the epoxy resin A is in the range of ≥ 0.9:1.

11. Composition according to Claim 10, characterized in that the stoichiometric ratio of the reactive groups of hardener H to the reactive groups of hardener B is in the range of ≥ 1:1.

12. Composition according to Claim 10, characterized in that the hardener H is a polymer having amino or carboxyl groups, wherein the polymer is selected from the group consisting of polyolefin, polyether, polyester, fatty acid, fatty acid amide and acrylonitrile-butadiene rubber with an acrylonitrile proportion of ≥ 25 mol%.

13. Composition according to Claim 12, characterized in that the hardener H is a polyether polyamine.

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